View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 15369U 84111A 23161.00695617 .00007159 00000-0 29608-3 0 9996
2 15369 82.5241 128.6109 0012847 220.1345 139.8944 15.23725803111607
| Epoch (UTC): | 10 June 2023 00:10:01 |
| Eccentricity: | 0.0012847 |
| inclination: | 82.5241° |
| perigee height: | 486 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 128.6109° |
| argument of perigee: | 220.1345° |
| revolutions per day: | 15.23725803 |
| mean anomaly at epoch: | 139.8944° |
| orbit number at epoch: | 11160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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